THE LAMINAR BOUNDARY LAYER IN COMPRESSIBLE FLOW

[1] Gas flow with laminary barriers along a plate [J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1935, 15 : 23 - 25

[2] COPE WF, 1942, REP MEMOR AERO RES C, V1903

[3] COPPLE C, 1938, J I ELECT ENG, V85, P56

[4] COWLING TG, 1947, IN PRESS

[5] A practical method for numerical evaluation of solutions of partial differential equations of the heat-conduction type [J]. ADVANCES IN COMPUTATIONAL MATHEMATICS, 1996, 6 (3-4) : 207 - 226

[6] CROCCO L, 1939, ATTI GUIDONIA, V17

[7] ECKERT E, 1940, FORSCH INGENIEURWES, V11, P116

[8] EMMONS HW, 1941, T ASME, V63, P105

[9] EMMONS HW, 1942, T AM SOC MECH ENG A, V64, P1

[10] Goldstein S., 1938, MODERN DEV FLUID DYN

[1] Gas flow with laminary barriers along a plate [J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1935, 15 : 23 - 25

[2] COPE WF, 1942, REP MEMOR AERO RES C, V1903

[3] COPPLE C, 1938, J I ELECT ENG, V85, P56

[4] COWLING TG, 1947, IN PRESS

[5] A practical method for numerical evaluation of solutions of partial differential equations of the heat-conduction type [J]. ADVANCES IN COMPUTATIONAL MATHEMATICS, 1996, 6 (3-4) : 207 - 226

[6] CROCCO L, 1939, ATTI GUIDONIA, V17

[7] ECKERT E, 1940, FORSCH INGENIEURWES, V11, P116

[8] EMMONS HW, 1941, T ASME, V63, P105

[9] EMMONS HW, 1942, T AM SOC MECH ENG A, V64, P1

[10] Goldstein S., 1938, MODERN DEV FLUID DYN